MIL-F-1183 (NOTICE 1), MILITARY STANDARD WELDING, GAS. STEELS, CONSTRUCTIONAL, READILY WELDABLE, FOR LOW-STRESSED JOINTS (9 JUL 1996) (S/S BY AWS-D1.3Ident. Num:
MIL-F-1183
Rev. Num:
-
MIL-F-1183 (NOTICE 1), MILITARY STANDARD WELDING, GAS. STEELS, CONSTRUCTIONAL, READILY WELDABLE, FOR LOW-STRESSED JOINTS (9 JUL 1996) (S/S BY AWS-D1.3)., MIL-STD-1183(AT), dated 12 December 1978, is hereby cancelled. Future acquisitions
should refer to American Welding Society (AWS) D 1.3 “Structural Welding Code-Sheet Steel”.
MIL-F-1183, MILITARY STANDARD WELDING, GAS. STEELS, CONSTRUCTIONAL, READILY WELDABLE, FOR LOW-STRESSED JOINTS (12 DEC 1978)Ident. Num:
MIL-F-1183
Rev. Num:
-
MIL-F-1183, MILITARY STANDARD WELDING, GAS. STEELS, CONSTRUCTIONAL, READILY WELDABLE, FOR LOW-STRESSED JOINTS (12 DEC 1978)., This standard covers oxy-acetylene gas welding of readily weldable constructional steels when joint strength is not a consideration in the function of the part.
MIL-F-14256F (AMENDMENT 1), MILITARY SPECIFICATION FLUX, SOLDERING, LIQUID, PASTE FLUX, SOLDER PASTE AND SOLDER-PASTE FLUX, (FOR ELECTRONIC/ELECTRICAL USE), GENERAL SPECIFICATION FOR (18 MAY 1994) [S/S BY J-STD-004, J-STD-005 AND J-STD-006]Ident. Num:
MIL-F-14256
Rev. Num:
F
MIL-F-14256F (AMENDMENT 1), MILITARY SPECIFICATION FLUX, SOLDERING, LIQUID, PASTE FLUX, SOLDER PASTE AND SOLDER-PASTE FLUX, (FOR ELECTRONIC/ELECTRICAL USE), GENERAL SPECIFICATION FOR (18 MAY 1994) [S/S BY J-STD-004, J-STD-005 AND J-STD-006].
MIL-F-14256F, MILITARY SPECIFICATION FLUX, SOLDERING, LIQUID, PASTE FLUX, SOLDER PASTE AND SOLDER-PASTE FLUX, (FOR ELECTRONIC/ELECTRICAL USE), GENERAL SPECIFICATION FOR (26 APR 1993) [S/S BY J-STD-004, J-STD-005 AND J-STD-006]Ident. Num:
MIL-F-14256
Rev. Num:
F
MIL-F-14256F, MILITARY SPECIFICATION FLUX, SOLDERING, LIQUID, PASTE FLUX, SOLDER PASTE AND SOLDER-PASTE FLUX, (FOR ELECTRONIC/ELECTRICAL USE), GENERAL SPECIFICATION FOR (26 APR 1993) [S/S BY J-STD-004, J-STD-005 AND J-STD-006]., This specification covers liquid fluxes, paste flux and solder-past flux used in the preparation of solder joints for electrical/electronic circuits.
MIL-F-17874B, MILITARY SPECIFICATION FUEL SYSTEMS, AIRCRAFT, INSTALLATION AND TEST OF (20 AUG 1965)Ident. Num:
MIL-F-17874
Rev. Num:
B
MIL-F-17874B, MILITARY SPECIFICATION FUEL SYSTEMS, AIRCRAFT, INSTALLATION AND TEST OF (20 AUG 1965)., This specification covers the general requirements for functional operation, installation, and testing of fuel systems for all piloted aircraft, target drones and guided missiles, and shall be followed except as otherwise authorized by the procuring activity for each design.
MIL-F-18240E, DETAIL SPECIFICATION FASTENER ELEMENT, SELF-LOCKING, THREADED FASTENER, 250°F MAXIMUM (1 DEC 1989) [S/S BY MIL-DTL-18240F)Ident. Num:
MIL-F-18240
Rev. Num:
E
MIL-F-18240E, DETAIL SPECIFICATION FASTENER ELEMENT, SELF-LOCKING, THREADED FASTENER, 250°F MAXIMUM (1 DEC 1989) [S/S BY MIL-DTL-18240F)., This specification defines the requirements for self-locking elements for use in
externally threaded fasteners such as bolts and screws to be used in fasteners with either UNC,
UNJC, UNF, UNJF, UNRC or UNRF threads and where the temperatures will not exceed 250°F.
MIL-F-19700A (SH), MILITARY SPECIFICATION FASTENERS, SCREW THREADED, AND RELATED ITEMS, NON-MAGNETIC (12 NOV 1987)Ident. Num:
MIL-F-19700
Rev. Num:
A
MIL-F-19700A (SH), MILITARY SPECIFICATION FASTENERS, SCREW THREADED, AND RELATED ITEMS, NON-MAGNETIC (12 NOV 1987)., This specification describes the characteristics of nonmagnetic,
screw threaded fasteners and related items that are dimensionally in conformance
to recognized Military and industrial standards. The intent of this specification
is to supplement,not supersede,the specifications normally used for the
acquisition of threaded fasteners and related items
MIL-F-495E (AMENDMENT 1), MILITARY SPECIFICATION FINISH, CHEMICAL, BLACK, FOR COPPER ALLOYS (5 FEB 1990)Ident. Num:
MIL-F-495
Rev. Num:
E
MIL-F-495E (AMENDMENT 1), MILITARY SPECIFICATION FINISH, CHEMICAL, BLACK, FOR COPPER ALLOYS (5 FEB 1990)., This amendment forms a part of MIL-F-495, dated 30 SEPTEMBER 1988, and is approved for use by all Departments and Agencies of the Department of Defense
MIL-F-495E (NOTICE 1), MILITARY SPECIFICATION FINISH, CHEMICAL, BLACK, FOR COPPER ALLOYS (24 SEPT 1999)Ident. Num:
MIL-F-495
Rev. Num:
E
MIL-F-495E (NOTICE 1), MILITARY SPECIFICATION FINISH, CHEMICAL, BLACK, FOR COPPER ALLOYS (24 SEPT 1999)., MIL-F-495E, including Amendment 1, dated 5 February 1990, is
hereby canceled without replacement.
MIL-F-495E (NOTICE 2), MILITARY SPECIFICATION FINISH, CHEMICAL, BLACK, FOR COPPER ALLOYS (19 JAN 2001)Ident. Num:
MIL-F-495
Rev. Num:
E
MIL-F-495E (NOTICE 2), MILITARY SPECIFICATION FINISH, CHEMICAL, BLACK, FOR COPPER ALLOYS (19 JAN 2001)., MIL-F-495E, including Amendment 1, dated 5 February 1990, is hereby reinstated and may be
used for acquisition.
MIL-F-5509D (NOTICE 1), MILITARY SPECIFICATION FITTINGS, FLARED TUBE, FLUID CONNECTION (20 DEC 1996) [SUPERSEDING MIL-L-5509C] [SEE NOTICE 2 FOR ADDITIONAL SUPERSEDING INFORMATION]Ident. Num:
MIL-F-5509
Rev. Num:
D
MIL-F-5509D (NOTICE 1), MILITARY SPECIFICATION FITTINGS, FLARED TUBE, FLUID CONNECTION (20 DEC 1996) [SUPERSEDING MIL-L-5509C] [SEE NOTICE 2 FOR ADDITIONAL SUPERSEDING INFORMATION]., MIL-F-5509D(4), dated 30 November 1987; and MIL-F-5509D, Supplement 1, dated
16 June 1978, are hereby canceled. Future acquisitions for these products should refer to
the following standard(s) as applicable to the specific fittings. Each replacement standard
cites superseding information for known fittings that have MIL-F-5509 designated as a
procurement specification:
MIL-F-5509D (NOTICE 2), MILITARY SPECIFICATION FITTINGS, FLARED TUBE, FLUID CONNECTION (30 SEP 1998) [SUPERSEDING MIL-L-5509C] [SEE NOTICE 2 FOR ADDITIONAL SUPERSEDING INFORMATION]Ident. Num:
MIL-F-5509
Rev. Num:
D
MIL-F-5509D (NOTICE 2), MILITARY SPECIFICATION FITTINGS, FLARED TUBE, FLUID CONNECTION (30 SEP 1998) [SUPERSEDING MIL-L-5509C] [SEE NOTICE 2 FOR ADDITIONAL SUPERSEDING INFORMATION]., MIL-F-5509D(4), dated 30 November 1987; and MIL-F-5509D, Supplement 1, dated
16 June 1978, are hereby canceled. Future acquisitions for these products should refer to the
following standard(s) as applicable to the specific fittings. Each replacement standard cites
superseding information for known fittings that have MIL-F-5509 designated as a procurement
specification. The attached cross-reference listing is provided to indicate which AN or MS from
MIL-F-5509D, Supplement 1, applies to the superseding procurement specifications.
MIL-F-7417, MILITARY SPECIFICATION FIXED GUN AND ROCKET INSTALLATIONS, ENGINEERING TEST OF (22 JUL 1954)Ident. Num:
MIL-F-7417
Rev. Num:
-
MIL-F-7417, MILITARY SPECIFICATION FIXED GUN AND ROCKET INSTALLATIONS, ENGINEERING TEST OF (22 JUL 1954)., This specification covers the requirements for the fabrication of a firing test stand and the engineering tests of fixed gun and rocket installations of new model military aircraft and succeeding models therof in which the installation has been re-designed, and any alternate installations thereof.
MIL-F-85720, FITTINGS, TUBE, FLUID SYSTEMS, SEPARABLE, HIGH PRESSURE, DYNAMIC BEAM SEAL, GENERAL SPECIFICATION FOR (17 JUN 1985) (S/S BY SAE-AS85720)Ident. Num:
MIL-F-85720
Rev. Num:
-
MIL-F-85720 (AS), FITTINGS, TUBE, FLUID SYSTEMS, SEPARABLE, HIGH PRESSURE, DYNAMIC BEAM SEAL, GENERAL SPECIFICATION FOR (17 JUN 1985) (S/S BY SAE-AS85720)., This specification covers the basic test and design
requirements for one style separable high pressure beam seai fittings
tnciuding boss or port seal connectors for use in 5000/8000 psi aerospace
fluid systems.
MIL-F-8785C, MILITARY SPECIFICATION FLYING QUALITIES OF PILOTED AIRPLANES (5 NOV 1980)Ident. Num:
MIL-F-8785
Rev. Num:
C
MIL-F-8785C, MILITARY SPECIFICATION FLYING QUALITIES OF PILOTED AIRPLANES (5 NOV 1980)., This specification contains the requirements for the flying and handling qualities, in
flight and on the ground, of U.S. Military, manned, piloted airplanes except for flight at airspeeds
below Vcon (MIL-F-83300). It is intended to assure flying qualities that provide adequate mission
performance and flight safety regardless of design implementation or flight control system
mechanization. The structure of the specification allows its use to guide these aspects in design
tradeoffs, analyses and tests.
MIL-F-9490D, FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT GENERAL SPECIFICATION FOR (6 JUN 1975)Ident. Num:
MIL-F-9490
Rev. Num:
D
MIL-F-9490D, FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT GENERAL SPECIFICATION FOR (6 JUN 1975)., This specification establishes general performance, design, development and quality assurance requirements for the flight control systems of USAF manned piloted aircraft. Flight control systems (FCS) include all components used to transmit flight control commands from the pilot or other sources to appropriate force and moment producers. Flight control commands may result in control of aircraft flight path, attitude, airspeed, aero dynamic configuration, ride, and structural modes. Among components included are the pilot's controls, dedicated displays and logic switching, transducers, system dynamic and air data sensors, signal computation, test devices, transmission devices, actuators, and signal transmission lines dedicated to flight control. ExcIuded are aerodynamic surfaces, engines, helicopter rotors, fire control devices, crew displays and electronics not dedicated to flight control. The interfaces of flight control systems with related subsystems are defined.
